Three dimensional printed precision magnets for fuel assembly

ABSTRACT

An improved retention and alignment system for nuclear fuel rods includes an upper nozzle plate and a lower nozzle plate, nuclear fuel rods, each having an upper end and a lower end and extending axially between the upper and lower nozzle plates, a first precision magnet incorporated onto the lower end of the fuel rod, and a plurality of second precision magnets incorporated onto the lower nozzle plate in positions confronting the first precision magnets on the fuel rods. Each first precision magnet has at least one of a magnetic north or south polarity and the second precision magnet has at least one of a magnetic south or north polarity opposite the polarity of the confronting first precision magnet to effect magnetic attraction between the confronting first and second precision magnets. Grids between the upper and lower nozzle plates form cells through which the fuel rods pass. Precision magnets of the same polarity may be positioned laterally along the fuel rods and grid walls in positions confronting each other to repel the fuel rods from the grid walls to maintain fuel rod alignment and prevent contact between the fuel rods and the grids.

CROSS-REFERENCE TO RELATED APPLICATIONS

This application is a divisional application claiming priority under 35U.S.C. § 121 to U.S. patent application Ser. No. 15/896,473, entitledTHREE DIMENSIONAL PRINTED PRECISION MAGNETS FOR FUEL ASSEMBLY, whichclaims benefit under 35 U.S.C. § 119 (e) to U.S. Provisional ApplicationNo. 62/464,457, filed Feb. 28, 2017, entitled THREE DIMENSIONAL PRINTEDPRECISION MAGNETS FOR FUEL ASSEMBLY, the entire disclosures of which arehereby incorporated by reference herein.

BACKGROUND OF THE INVENTION 1. Field of the Invention

The present invention relates to retention systems for nuclear fuelrods, and more particularly to magnetic retention systems.

2. Description of the Prior Art

In conventional nuclear reactor systems, the fuel rods are held inposition axially and laterally with mechanical components such assprings, braces, end plugs, and other devices positioned along thelength and at each end of a fuel rod. Such traditional means ofretention and alignment sacrifice system pressure without providing acorresponding thermal efficiency benefit. The flow of fluid coolantaround the fuel rods past the mechanical retention and alignmentcomponents reduces the coolant pressure causing a pressure drop in thecoolant flow.

Further, the retention and alignment components may cause wear of thefuel rods due to contact between the structural retention features andthe fuel, which may lead to fuel rod damage.

Elimination of these retention and alignment contact features wouldeliminate or reduce the coolant pressure drop. Avoiding loss of pressurewould increase fuel efficiency.

SUMMARY OF THE INVENTION

The problems associated with physical contact-based retention andalignment features are addressed by the system for retention andalignment of nuclear fuel rods described herein wherein retention isachieved by magnetizing certain contacts between adjacent components.Magnetization may be achieved by using precision magnets keyed to thepolarity of confronting precision magnets.

An improved retention and alignment system for nuclear fuel rods may, invarious aspects, include an upper plate and a lower nozzle, at least onenuclear fuel rod having an upper end and a lower end and extendingaxially between the upper and lower nozzles, a first precision magnetincorporated onto the lower end of the at least one fuel rod, and, asecond precision magnet incorporated onto the lower nozzle in a positionconfronting the at least one first precision magnet. The first precisionmagnet has at least one of a magnetic north or south polarity and thesecond precision magnet has at least one of a magnetic south or northpolarity opposite the polarity of the confronting first precision magnetto effect magnetic attraction between the confronting first and secondprecision magnets.

In various aspects, there is a first precision magnet incorporated ontothe lower ends of the at least one fuel rod and a second precisionmagnet incorporated onto the lower nozzle to axially retain the fuel rodbetween the upper and lower nozzles by magnetic attraction.

In various aspects of the system, each of the at least one first andsecond precision magnets has at least one, and in certain aspects, twoor more, paired sections. Each paired section has a polarity oppositethe other section in the pair. The paired sections may be configured ina locked configuration wherein confronting precision magnet sectionsattract each other to an unlocked configuration wherein confrontingprecision magnet sections repel each other.

In various aspects, the polarity of each member of the pair may beselectively switchable, for example by rotation, to the oppositepolarity to selectively switch one of the first or second precisionmagnets from the locked configuration to the unlocked configuration. Invarious aspects of the system, the paired sections of at least one ofthe first and second precision magnets may be rotatable for rotating thepaired sections of one of the first and second magnets into the lockedor the unlocked configuration.

The improved retention and alignment system may address problems ofmaintaining fuel rod alignment during seismic events. The system mayinclude at least one grid substantially parallel to and positionedbetween the upper and lower nozzles. The at least one grid defines aperimeter and has within the perimeter, a first set of grid strapextending laterally and longitudinally across the grid to define atleast one, and in various aspects, multiple cells. Each cell has aninterior and an exterior, wherein one of the at least one fuel rodspasses axially through the interior of one cell. The grid strap walls ofthe grid may include at least one third precision magnet incorporatedonto the interior of the cell. At least one fourth precision magnet maybe incorporated onto a side of the fuel rod, fuel rod cladding, or asleeve over the fuel rod in a position confronting the at least onethird precision magnet. The third precision magnet has at least one of amagnetic north or south polarity and the fourth precision magnet has atleast one of a magnetic north or south polarity the same as the polarityof the confronting third precision magnet to effect magnetic repulsionbetween the confronting third and fourth precision magnets formaintaining a gap between the fuel rod and the grid strap onto which theconfronting third precision magnet is incorporated.

The system may have in certain aspects, a plurality of cells and aplurality of fuel rods, wherein each cell is sized to receive one of theplurality of fuel rods extending axially therethrough.

In various aspects, each enclosure through which a fuel rod passes hasat least two third precision magnets incorporated onto different gridstrap walls of the enclosure and the fuel rod (or its cladding orsleeve) has at least two fourth precision magnets. Each fourth precisionmagnet is positioned on the fuel rod to confront a different one of theat least two third precision magnets incorporated onto the grid strapwalls.

BRIEF DESCRIPTION OF THE DRAWINGS

The characteristics and advantages of the present disclosure may bebetter understood by reference to the accompanying figures.

FIG. 1 is a cut-away perspective view of some of the components of aconventional fuel assembly showing a control rod assembly, a top nozzle,several grid layers, a bottom nozzle, fuel rods and grid sleeves.

FIGS. 2A and 2B illustrate the difference between the magnetic fieldlines in a conventional magnet (FIG. 2A) and a precision magnet (FIG.2B), showing the loss experienced with conventional magnets.

FIG. 3 is a view of prior art precision magnets with a patterned printed“locking/resistance” design, showing positive and negative polesdistributed over the surface of the magnets.

FIG. 4 is a view of the magnetic fields visible under a magnetic filmshowing positive and negative poles patterned over the surface of priorart discs.

FIG. 5A shows an end of a fuel rod having paired sections of precisionmagnets printed thereon.

FIG. 5B shows a bottom plate having a retention member comprised ofpaired sections of precision magnets opposite in polarity to theconfronting fuel rod sections printed thereon for magnetically retainingthe fuel rod of FIG. 5A.

FIG. 6 is a view of the end of the fuel rod of FIG. 5A mating with theprecision magnet retention member of FIG. 5B in a locked position whereconfronting sections are of the opposite polarity.

FIG. 7 is a view of the fuel rod and precision magnet retention memberof FIG. 6 in an unlocked position where the confronting sections are ofthe same polarity.

FIG. 8 is a perspective view of an alternative embodiment of a portionof a bottom plate showing printed end plug precision magnet contacts formating engagement with a precision magnet on the end of a fuel rod ofFIG. 5A.

FIG. 9 is a partial view of an embodiment of a grid strap wall for afuel rod, showing precision magnets printed the exterior of a grid strapwall to create impact resistance between adjacent grid strap surfaces ata desired gap.

FIG. 10 is a partial perspective view of adjacent grid strap walls ofFIG. 9 showing precision magnets on the exterior surface of each gridstrap wall.

FIG. 11 is a top plan view of fuel rods in an embodiment of a gridassembly showing both precision magnets and stabilizing dimples forlateral positioning of the fuel rods.

FIG. 12 is a perspective view of the fuel rod assembly of FIG. 11 .

FIG. 13 is a top plan view of fuel rods in an alternative embodiment ofa grid assembly showing only precision magnets on the interior of theenclosure and the fuel rod for lateral positioning of the fuel rods.

FIG. 14 is a perspective view of the fuel rod assembly of FIG. 13 .

DESCRIPTION OF THE PREFERRED EMBODIMENTS

As used herein, the singular form of “a”, “an”, and “the” include theplural references unless the context clearly dictates otherwise. Thus,the articles “a” and “an” are used herein to refer to one or to morethan one (i.e., to at least one) of the grammatical object of thearticle. By way of example, “an element” means one element or more thanone element.

Directional phrases used herein, such as, for example and withoutlimitation, top, bottom, left, right, lower, upper, front, back, andvariations thereof, shall relate to the orientation of the elementsshown in the accompanying drawing and are not limiting upon the claimsunless otherwise expressly stated.

In the present application, including the claims, other than whereotherwise indicated, all numbers expressing quantities, values orcharacteristics are to be understood as being modified in all instancesby the term “about.” Thus, numbers may be read as if preceded by theword “about” even though the term “about” may not expressly appear withthe number. Accordingly, unless indicated to the contrary, any numericalparameters set forth in the following description may vary depending onthe desired properties one seeks to obtain in the compositions andmethods according to the present disclosure. At the very least, and notas an attempt to limit the application of the doctrine of equivalents tothe scope of the claims, each numerical parameter described in thepresent description should at least be construed in light of the numberof reported significant digits and by applying ordinary roundingtechniques.

Further, any numerical range recited herein is intended to include allsub-ranges subsumed therein. For example, a range of “1 to 10” isintended to include any and all sub-ranges between (and including) therecited minimum value of 1 and the recited maximum value of 10, that is,having a minimum value equal to or greater than 1 and a maximum value ofequal to or less than 10.

An exemplary nuclear reactor fuel rod and coolant system 10 is shown inpart in FIG. 1 . The system 10 includes a control rod assembly 12positioned at the upper end of the system 10, a top nozzle 14 with leafsprings 16, a top nozzle plate 28, a bottom nozzle 22, bottom nozzleplate 30, and several grids 68, 88, and 18 positioned between the topand bottom nozzle plates 28, 30 to support rows of fuel rods 20extending between the top and bottom nozzles plates 28, 30. Theplurality of grids 68, 88, and 18 are substantially parallel to, butseparated from each other, and supported by support rods 24, sometimesreferred to as guide thimbles, positioned inside the grid perimeter andinside several rows of fuel rods 20. Cut-away sections of FIG. 1 show apattern of holes 26 through each of a top grid 68, mid-grid 88, andbottom grid 18 through which the fuel rods 20 pass from the bottomnozzle plate 30 to the top nozzle plate 28. Holes 26 are sized to allowcoolant fluid flow around the fuel rods 20. Additional openings, forexample, venturi openings, may be formed in the top and bottom nozzlesplates 28, 30. The system 10 is enclosed in a reactor housing (notshown).

As stated above, in conventional nuclear reactor systems, the fuel rods20 are held in position laterally with springs 48 and/or dimples 58 onthe inner sides of the grids 68, 88, and 18. In a typical conventionalsystem, each cell has two dimples and two springs. Both the dimples andthe springs arch into the cell from the grid strap wall forming raisedportions 56 for contact with the fuel rod 20. The more flexible spring48 forces the fuel rod against the raised portion 56 of the dimple 58 tolaterally secure the rod within the cell. The flow of fluid coolantaround the fuel rods 20 past the springs 48 and other retention featuresto retain the fuel rods 20 and supports 24 in position reduces thecoolant pressure causing a pressure drop in the coolant flow.

In the retention system described herein, fuel rods 20 are held inposition using keyed patterns of confronting precision magnets. Themethods of axial and lateral fuel rod retention described hereinprovides opportunities to eliminate components, reduce aforementionedpressure drop, and improve grid to rod fretting (e.g., reduce oreliminate wear of the fuel rods due to contact with structural retentionfeatures of the grid). By incorporating a means of dampening orpreventing adjacent fuel assembly impact with features of grids 68, 88,and 18, the improved retention and alignment system will reduce seismicforces on the fuel assemblies and reduce, and preferably, eliminate therisk of associated loss-of-coolant accidents. The improved retention andalignment system will also prevent fuel assembly lift off at the axialretention features, and allow for easier removal of components forreconstitution, repair or replacement.

Precision magnets are fundamentally different than conventional magnets.Most off the shelf conventional magnets have a simple configuration: anorth pole on one side and a south pole on the other. Software-drivenmagnetizers, such as those sold under the mark, POLYMAGNETS®, byCorrelated Magnetics Research LLC of California, USA, have beencommercially developed that enable manufacture of customizable patternsof magnetism designed in software and programmed into a magnet. See, forexample, U.S. Pat. Nos. 8,179,219; 9,219,403; 9,245,677 and 9,404,776,incorporated in relevant part herein by reference. These precisionmagnets can be up to five times stronger than conventional magnetsbecause their magnetic energy may be concentrated near the surface, asshown in FIG. 2 . 3-D printed precision magnet technology is an emergingfield that prints individual (digital/pixelated) magnetic poles intocustomizable orientations and 3-D geometries. This ability to printsmall field magnetic circuits allows for increased magnetic forces overa smaller distance due to the reduced energy loss of the field.Conventional magnets 206, 208 as shown in FIG. 2A do not necessarilyalign when attaching to each other. The magnetic field lines 210 ofconventional magnets 206, 208 show that much of the magnetic energy islost, directed away from the magnets 206, 208. Precision magnets, asshown in FIG. 2B, concentrate the magnetic field. The magnetic fieldlines 210 in the precision magnets 202, 204, form a smaller, tighterfield so that the magnetic force remains with the magnets.

Precision magnets, such as those sold under the mark, POLYMAGNETS®, maybe designed to align with a wide variety of alignment functions. Latchprecision magnets, for example, are designed to repel until the magnetpair pass through a defined transition point. After the transition pointthey are designed to reverse polarity and attract. Spring precisionmagnets are designed to attract until they pass through a definedtransition point, past which they will repel. These precision magnetswill come to rest at an equilibrium distance. At equilibrium, theopposing precision magnets maintain a predetermined distance from eachother so that the components into which the precision magnets are placedcan be held apart, spaced from each other at or about the predetermineddistance.

Referring to FIGS. 3 and 4 , variations in precision magnetconfigurations are shown for illustration purposes. In FIG. 3 , twoopposing discs 200 are shown having a plurality of precision magnets oneach disc keyed to the precision magnets on the confronting disc.Precision magnets having, for example, a north magnetic pole 202 areshown with a plus sign and precision magnets having a south magneticpole 204 are shown with a negative sign. When discs A and B are movedtoward each other, they can be aligned so that the north (+) poles ondisc A directly align with the south (−) poles on disc B, and the south(−) poles on disc A align with the north (+) poles on disc B, forcingthe discs A and B to attract and join together. Because of the tightmagnetic field, as shown in FIG. 2B, the force of attraction betweendiscs A and B is very strong. If it is necessary or desirable to havethe two discs 200 repel each other, the precision magnets 202, 204 onthe discs 200 may be aligned so that the north (+) and south (−) poleson disc A align with the north (+) and south (−) poles, respectively, ondisc B. The like magnetic poles on opposing discs will repel each other,forcing the discs A and B apart. In FIG. 3 , an image of two discs 200placed side-by-side show the magnetic fields of the discs through asheath 300. The disc on the right side of the image has precisionmagnets having (+) poles 202 on the outer ring and precision magnetshaving (−) poles 204 in a center ring. The disc 200 on the left side ofthe image has precision magnets 202, 204 with alternating north (+) andsouth (−) poles, respectively. FIGS. 3 and 4 illustrate the possiblegeometries and patterns that may be used in configuring precision magnetretention assemblies.

Keyed confronting precision magnets for use in the environment of anuclear fuel and coolant system 10 may be made of any suitable materialsthat are believed to retain their magnetic properties under reactorconditions. Research has shown that certain materials, such as Sm2Co17,have temperature and irradiation resistance with regard to degradationof magnetic properties.

The ability to axially secure and maintain the alignment of fuel rods 20by means of a non-lateral contact method, such as by use of precisionmagnets, may make it possible to eliminate the bottom grid 88, and wouldsignificantly reduce pressure drop penalties in current fuel designs.The retention geometries may be magnetically keyed to allow for easyfuel rod 20 reconstitution.

Referring to FIG. 5A, a modification of the conventional end plug 32design of a fuel rod 20 is shown. The end plug 32 includes a bosssection 38 that is welded to one or both of the ends of a fuel rod 20(not shown in this view). An end surface 34, for example, on the bottomend plug 32 may, in various aspects, have first precision magnets 36incorporated on the surface 34. The first magnets may be a single magnetof a single polarity. As shown, in certain aspects, the first magnet maycomprise paired sections of one or both positive and negativepolarities, such as the alternating positive (+) 202 and negative (−)204 pattern of poles shown on surface 34.

FIG. 5B shows the bottom nozzle plate 30 including a plurality of holes42 for passage of reactor coolant, such as water, around the fuel rods20 and feet 44 for supporting the bottom nozzle plate 30. Bottom nozzleplate 30 further includes a second precision magnet 40 incorporatedtherein for each fuel rod 20 for alignment with the first precisionmagnet 36 on end surface 34 of end plug 32 of fuel rod 20. The secondprecision magnet 40 may be a single magnet of a single polarity oppositethe polarity of the first single magnet 36, or may comprise pairedsections of one or both positive and negative polarities, as shown inFIG. 5B, able to be positioned or programmed such that the polarity ofthe paired sections on surface 34 are opposite the polarity of thepaired sections on nozzle plate 30. The second precision magnet 40includes alternating positive (+) 202 and negative (−) 204 poles that,when aligned in an orientation opposite that of the poles on the firstprecision magnet 36 on the end surface 34, exhibit strong magneticattraction, locking the fuel rod 20 in position on bottom nozzle plate30 when the two are brought into contact with each other, as shown inFIG. 6 . In various aspects, a similar end surface with a precisionmagnet 36 may be incorporated on the upper end of the fuel rod 20 formagnetic attachment to a mating precision magnet 40 incorporated intothe top nozzle plate 28. With precision magnets on the lower end of thefuel rods 20 in a confronting position relative to the bottom nozzleplate 30, the fuel rods 20 may be locked into axial alignment within thereactor system 10. When it is necessary to move a fuel rod 20, forexample, to reconstitute, replace or repair it, one of the first orsecond precision magnets 36, 40 on the end of the fuel rod 20 is turnedto position the positive (+) and negative (−) poles 202, 204 of oneprecision magnet 36 or 40 into alignment with the like poles of theopposing precision magnet 40 or 36 so that the bottom end surfaces ofthe fuel rod (or fuel rod end plug) and associated nozzle plate 30 repeleach other, moving into an unlocked position, as shown in FIG. 7 .

In certain aspects, each of the first and second precision magnets 36,40 may be formed from a plurality of paired sections, wherein eachsection of a pair may have the same polarity as the other section of thepair or each section of a pair may have the opposite polarity of theother section of the pair. The polarity of each section may beselectively switchable to the opposite polarity to selectively switchone of the first or second precision magnets 36, 40 from the lockedconfiguration wherein at least a majority of the confronting precisionmagnet sections attract each other to an unlocked position wherein atleast a the majority of the confronting precision magnet sections repeleach other. In this embodiment, the strength of the attractive orrepelling force may be controlled by polarities of confronting sectionsof the precision magnets.

In another aspect, as shown in FIG. 8 , a second precision magnet 40 maybe placed by suitable means, for example, by 3-D printing, in each of aplurality of spaced recessed portions 46 in a bottom nozzle plate 30′,also having holes 42 in the nozzle plate 30′ for coolant flow about eachfuel rod 20. The nozzle plate 30′ may, in certain aspects, have an eggcrate-like structure comprised of the plurality of recessed portions 46and coolant flow holes 42. Each such recessed portion 46 is configuredto seat the end plug 32 of one of a plurality of fuel rods 20. Theplurality of recessed portions 46 may include a floor section onto whicha second precision magnet 40 is incorporated and openings around thefloor that lead to venturi type openings directly below the recess 46for coolant flow. The flow holes 42 may also form venturi type openings.In use, the first precision magnet 36 on the end surface 34 of each endplug 32 is positioned to align with precision magnet 40 on the floor ofthe recessed portion 46 to either attract or repel each other forlocking or unlocking, respectively, the fuel rod 20 to the nozzle plate30′. The precision magnets 36, 40 may, as described above, have pairedsections of alternating patterns of positive (+) 202 and negative (−)204 poles on each of the precision magnets which may be rotated into anattracting or a repelling alignment, or each may have a single positive(+) 202 or negative (−) 204 pole on one and a single negative (−) 204 orpositive (+) 202 pole on the other, opposite the polarity of theconfronting precision magnet, to attract each other to axially lock thefuel rod 20 into the recessed portion 46. Unlocking may occur byreversing the polarity of one of the two confronting precision magnets,for example, by rotating the fuel rod.

A conventional grid includes laterally positioned grid straps 50 thatcrisscross within the grid perimeter to define cells 60 through whichthe fuel rods 20 pass. The grid straps 50 serve to align the fuel rods20 laterally and prevent adjacent fuel rods 20 from contacting eachother. The grid straps 50 may include springs 48. The embodiment ofexemplary springs 48 is shown in FIGS. 9-10 . Each cell 60 may includeone or two springs 48, on different sides of the grid strap sectionsthat define the cell 60. In various embodiments, each cell may includetwo springs 48 or two dimples 58. The springs 48 or dimples 58 extend orarch from the grid strap wall into the cell 60 forming a raised plateau56 which bows toward the fuel rod 20 when the rod is positioned withincell 60 such that the elevated plateau 56 of spring 48 is pressed orwedged laterally against the adjacent fuel rod 20. The springs 48 may bearranged so that at least two plateaus 56 extend into each cell 60 tolaterally secure the rod 20 within the cell 60.

In certain aspects, when there are adjacent fuel assemblies 10, the griddesign may include a first set of grid straps 50 on the perimeter of onefuel assembly 10 and a second set of grid straps 52 on the perimeter ofthe adjacent fuel assembly 10 on each grid 68, 88, and 18. The secondset of grid straps 52 are positioned adjacent the first set of gridstraps 50 to define a space between adjacent grid strap walls 50, 52.Adjacent grid strap walls are positioned in planes substantiallyparallel and spaced from each other.

In certain aspects, shown in FIGS. 9 and 10 , precision magnets 361 and401, keyed to precision magnets 362 and 402, may be incorporated intothe exterior surfaces of adjacent grid straps 50, 52 of the first andsecond sets for lateral impact dampening to maintain a distance betweenthe adjacent fuel assemblies 10. A novel grid design for accidenttolerant fuel configurations may add one or both sets of precisionmagnets 361, 362 and 401, 402, incorporating them into the outersurfaces of the grid straps 50, 52 during the manufacturing process.Manufacture of the grid straps 50, 52 may, for example, be by anysuitable known 3-D printing method or any other process for forming amolded three dimensional product or surface. Precision magnet patternsmay be printed, for example, into the adjacent areas of grid straps 50,52 to create resistance at a pre-determined distance or gap 54 betweenthe outer sides of adjacent grid straps 50, 52. The gaps 54 reduceseismic and loss of coolant accident forces without the need forexternal features on the grid straps that may cause damage to the fuelrods 20 held within the cells 60 in the event of unplanned movement ofany significant force. When each aligned pole 202 or 204 of the opposingprecision magnets 361, 362 and 401, 402, respectively, is of the samepolarity, the grid straps 50, 52 will repel each other and resistimpact. By controlling the strength of the magnetic field generated bythe precision magnets 361, 362, 401 and/or 402, the distance 54 betweenthe exteriors of adjacent grid straps 50, 52 can be controlled andmaintained under adverse conditions.

Referring to FIGS. 11-12 , an alternative fuel rod lateral positioningconfiguration is shown that incorporates precision magnets 72 into theinside of the cells 60 and confronting precision magnets 70 on the fuelrods 20. Precision magnet patterns may be incorporated into the interiorside of grid strap walls 50 in place of or in addition to dimples 58,which align fuel rods 20 within the grid cells 60. A thin sleeve 62 canbe attached to the fuel rod 20. The sleeve 62 may in various aspects, beprinted with the opposite magnetic pole from the pole incorporated intogrid strap 50 at some or all grid 68, 18, or 88 elevations within thesystem 10. As shown, the repelling force of the confronting like-poleprecision magnets (i.e., each of the confronting precision magnetshaving positive (+) poles 202 or each of the confronting precisionmagnets having negative (−) poles 204) maintains a desired gap 74between the fuel rod 20 or a sleeve covering the rods 20. Thisarrangement will provide a significant grid-to-rod fretting marginbecause there would be much less (if any) rod 20, 24 contact supportrequired.

Referring to FIG. 11 , cells 60 defined by grid straps 50 are shown inan alternative arrangement from the grid strap arrangement describedabove and shown in FIG. 10 . Each cell 60 also includes mixing vanes 78for controlling coolant flow around rods 20. Coolant flow runs parallelto the rods 20.

In certain aspects, as shown in FIGS. 13-14 , dimples 58 may beeliminated as a retention means from cells 60 so that precision magnets72 on the interior of grid straps 50 and precision magnets 70 on rod 20or a rod sleeve 62 provide the sole means of maintaining the separation,gap 74, between the rods 20 and grid straps 50 within each cell 60.

A significant cost savings can be gained by combining and eliminatingcomponents. Components can be more easily controlled and result in acost savings by removing tightly tolerance features such as springs anddimples in sheet metal components. There will be less pressure drop incoolant flow resulting in increased fuel efficiency and a higherburn-up. Movements between fuel assemblies and fuel rods that may occurin accident conditions can be better controlled, preventing damage dueto sudden impacts between adjacent components. The use of precisionmagnets for maintaining lateral rod position control provides contactfree retention. This provides more clearance between the fuel rods andother components, improving wear because debris will not be trappedagainst the fuel rods.

The improved retention features described herein create opportunities tosimplify structural components and, importantly, create safer fueldesigns for use in higher seismic locations.

The present invention has been described in accordance with severalexamples, which are intended to be illustrative in all aspects ratherthan restrictive. Thus, the present invention is capable of manyvariations in detailed implementation, which may be derived from thedescription contained herein by a person of ordinary skill in the art.

All patents, patent applications, publications, or other disclosurematerial mentioned herein, are hereby incorporated by reference in theirentirety as if each individual reference was expressly incorporated byreference respectively. All references, and any material, or portionthereof, that are said to be incorporated by reference herein areincorporated herein only to the extent that the incorporated materialdoes not conflict with existing definitions, statements, or otherdisclosure material set forth in this disclosure. As such, and to theextent necessary, the disclosure as set forth herein supersedes anyconflicting material incorporated herein by reference and the disclosureexpressly set forth in the present application controls.

The present invention has been described with reference to variousexemplary and illustrative embodiments. The embodiments described hereinare understood as providing illustrative features of varying detail ofvarious embodiments of the disclosed invention; and therefore, unlessotherwise specified, it is to be understood that, to the extentpossible, one or more features, elements, components, constituents,ingredients, structures, modules, and/or aspects of the disclosedembodiments may be combined, separated, interchanged, and/or rearrangedwith or relative to one or more other features, elements, components,constituents, ingredients, structures, modules, and/or aspects of thedisclosed embodiments without departing from the scope of the disclosedinvention. Accordingly, it will be recognized by persons having ordinaryskill in the art that various substitutions, modifications orcombinations of any of the exemplary embodiments may be made withoutdeparting from the scope of the invention. In addition, persons skilledin the art will recognize, or be able to ascertain using no more thanroutine experimentation, many equivalents to the various embodiments ofthe invention described herein upon review of this specification. Thus,the invention is not limited by the description of the variousembodiments, but rather by the claims.

1-15. (canceled)
 16. A retention and alignment system for a fuel rod,the retention and alignment system comprising: a first nozzle plate; asecond nozzle plate, wherein the fuel rod extends between the firstnozzle plate and the second nozzle plate; a grid positioned between thefirst nozzle plate and the second nozzle plate, wherein the gridcomprises a plurality of grid straps, and wherein the plurality of gridstraps define a cell comprising a first surface; a first precisionmagnet positioned on the first surface of the cell; and a secondprecision magnet positioned on the fuel rod, wherein the secondprecision magnet is configured to confront the first precision magnet togenerate a first repelling force therebetween to maintain a gap betweenthe fuel rod and the first surface of the cell.
 17. The retention andalignment system of claim 16, wherein the cell further comprises asecond surface, wherein the retention and alignment system furthercomprises a spring extending from the second surface, and wherein thefirst repelling force drives the fuel rod into engagement with thespring.
 18. The retention and alignment system of claim 16, wherein thecell further comprises a second surface, and wherein the retention andalignment system further comprises: a third precision magnet positionedon the second surface of the cell; and a fourth precision magnetpositioned on the fuel rod, wherein the fourth precision magnet isconfigured to confront the third precision magnet to generate a secondrepelling force therebetween to maintain a second gap between the fuelrod and the second surface of the cell.
 19. The retention and alignmentsystem of claim 18, wherein the first repelling force is along a firstaxis, and wherein the second repelling force is along a second axistransverse the first axis.
 20. The retention and alignment system ofclaim 18, wherein the cell further comprises a third surface, whereinthe retention and alignment system further comprises a spring extendingfrom the third surface, and wherein the first repelling force drives thefuel rod into engagement with the spring.
 21. The retention andalignment system of claim 18, wherein the cell further comprises a thirdsurface, and wherein the retention and alignment system furthercomprises: a fifth precision magnet positioned on the third surface ofthe cell; and a sixth precision magnet positioned on the fuel rod,wherein the sixth precision magnet is configured to confront the fifthprecision magnet to generate a third repelling force therebetween tomaintain a third gap between the fuel rod and the second surface of thecell.
 22. The retention and alignment system of claim 21, wherein thefirst repelling force is along a first axis, wherein the secondrepelling force is along a second axis transverse the first axis, andwherein the third repelling force is along a third axis transverse thesecond axis.
 23. The retention and alignment system of claim 16, whereinthe cell further comprises a mixing vane configured to control coolantflow around the fuel rod within the cell.
 24. A retention and alignmentsystem for a fuel rod, the retention and alignment system comprising: afirst nozzle plate; a second nozzle plate, wherein the fuel rod extendsbetween the first nozzle plate and the second nozzle plate; a gridpositioned between the first nozzle plate and the second nozzle plate,wherein the grid comprises a plurality of grid straps, and wherein theplurality of grid straps define a cell comprising a first surface; asleeve coupled to the fuel rod, wherein the sleeve comprises a polarity;and a precision magnet positioned on the first surface of the cell,wherein the precision magnet is configured to confront the sleeve togenerate a first repelling force between the precision magnet and thesleeve to maintain a gap between the fuel rod and the first surface ofthe cell.
 25. The retention and alignment system of claim 24, whereinthe cell further comprises a second surface, wherein the retention andalignment system further comprises a spring extending from the secondsurface, and wherein the first repelling force drives the fuel rod intoengagement with the spring.
 26. The retention and alignment system ofclaim 24, wherein the cell further comprises a second surface, whereinthe retention and alignment system further comprises a second precisionmagnet positioned on the second surface of the cell, and wherein thesecond precision magnet is configured to confront the sleeve to generatea second repelling force between the second precision magnet and thesleeve to maintain a second gap between the fuel rod and the secondsurface of the cell.
 27. The retention and alignment system of claim 26,wherein the first repelling force is along a first axis, and wherein thesecond repelling force is along a second axis transverse the first axis.28. The retention and alignment system of claim 26, wherein the cellfurther comprises a third surface, wherein the retention and alignmentsystem further comprises a spring extending from the third surface, andwherein the first repelling force drives the fuel rod into engagementwith the spring.
 29. The retention and alignment system of claim 26,wherein the cell further comprises a third surface, wherein theretention and alignment system further comprises a third precisionmagnet positioned on the third surface of the cell, and wherein thethird precision magnet is configured to confront the sleeve to generatea third repelling force between the third precision magnet and thesleeve to maintain a third gap between the fuel rod and the thirdsurface of the cell.
 30. The retention and alignment system of claim 29,wherein the first repelling force is along a first axis, wherein thesecond repelling force is along a second axis transverse the first axis,and wherein the third repelling force is along a third axis transversethe second axis.
 31. The retention and alignment system of claim 24,wherein the cell further comprises a mixing vane configured to controlcoolant flow around the fuel rod within the cell.
 32. A retention andalignment system for a fuel rod, the retention and alignment systemcomprising: a first nozzle plate; a second nozzle plate, wherein thefuel rod extends between the first nozzle plate and the second nozzleplate; a grid positioned between the first nozzle plate and the secondnozzle plate, wherein the grid comprises a plurality of grid straps,wherein the plurality of grid straps define a cell comprising a firstsurface and a second surface; a first precision magnet positioned on thefirst surface of the cell, wherein the first precision magnet isconfigured to interface with the fuel rod to generate a first repellingforce therebetween to maintain a first gap between the fuel rod and thefirst surface of the cell; and a second precision magnet positioned onthe second surface of the cell, wherein the second precision magnet isconfigured to interface with the fuel rod to generate a second repellingforce therebetween to maintain a second gap between the fuel rod and thesecond surface of the cell.
 33. The retention and alignment system ofclaim 32, wherein the cell further comprises a third surface, whereinthe retention and alignment system further comprises a third precisionmagnet positioned on the third surface of the cell, and wherein thethird precision magnet is configured to interface with the fuel rod togenerate a third repelling force therebetween to maintain a third gapbetween the fuel rod and the third surface of the cell.
 34. Theretention and alignment system of claim 32, wherein the cell furthercomprises a third surface, wherein the retention and alignment systemfurther comprises a spring extending from the third surface, and whereinthe first repelling force drives the fuel rod into engagement with thespring.
 35. The retention and alignment system of claim 32, wherein thecell further comprises a mixing vane extending toward the fuel rod,wherein the mixing vane is configured to control coolant flow around thefuel rod within the cell.